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    SUSPENDED LAYERED ENERGY ABSORBING MATERIAL FOR VEHICLE ARRESTING SYSTEMS
    1.
    发明申请
    SUSPENDED LAYERED ENERGY ABSORBING MATERIAL FOR VEHICLE ARRESTING SYSTEMS 审中-公开
    悬挂式能量吸收材料用于车辆装载系统

    公开(公告)号：WO2016187276A1

    公开(公告)日：2016-11-24

    申请号：PCT/US2016/033037

    申请日：2016-05-18

    Applicant: ENGINEERED ARRESTING SYSTEMS CORPORATION

    Inventor： DOHERTY, Shawn P. ,  FLYNN, Nicholas M. ,  SHI, Jack ,  MA, Sarah ,  ZOU, Hong

    IPC: B64F1/02 ,  E01C9/00

    CPC classification number: E01C9/007 ,  B64F1/025 ,  E01C19/00

    Abstract: Embodiments of the invention described herein thus provide systems and methods for arresting aircraft. In specific embodiments, the systems and methods can be useful in arresting light aircraft because they typically do not have the weight to penetrate available EMAS systems. The system is generally provided as a structure having a suspended layer of energy absorbing material. A lower portion of the system can have a lower strength, used as a method to suspend an upper, stronger/more highly energy absorbent portion of the system.

    Abstract translation: 因此，本文描述的本发明的实施例提供了用于制动飞行器的系统和方法。 在具体实施例中，系统和方法可用于阻止轻型飞行器，因为它们通常不具有穿透可用的EMAS系统的重量。 该系统通常被提供为具有悬浮层的能量吸收材料的结构。 系统的下部可以具有较低的强度，用作悬挂系统的上部，更强/更高能量吸收部分的方法。

    POLYMERIC FOAM COMPOSITE FOR VEHICLE ARRESTING SYSTEM
    2.
    发明申请
    POLYMERIC FOAM COMPOSITE FOR VEHICLE ARRESTING SYSTEM 审中-公开
    用于车辆收集系统的聚合物泡沫复合材料

    公开(公告)号：WO2016100676A1

    公开(公告)日：2016-06-23

    申请号：PCT/US2015/066395

    申请日：2015-12-17

    Applicant: ENGINEERED ARRESTING SYSTEMS CORPORATION

    Inventor： VALENTINI, Silvia, C. ,  ZOU, Hong ,  GALBUS, Michael, T. ,  FLYNN, Nicholas, M.

    IPC: C08J9/34 ,  C08J9/36 ,  E01C9/00 ,  B64F1/02

    CPC classification number: B64F1/025 ,  C08J9/34 ,  C08J9/365 ,  C08J2205/08 ,  C08J2325/06 ,  E01C9/007

    Abstract: Embodiments of the present invention relate to composite materials for use as a vehicle arresting system (also referred to as an Engineered Material Arresting System (EMAS). Specific embodiments may use modified polymeric foams composites. The polymeric foams may include additives, coatings, combinations of both, or other features than render them useful for an EMAS. The polymeric foams may also have one or more modified surfaces that provide a protective crust. For example, the one or more surface may be modified by application of heat in order to help close the polymeric foam cells and/or to create an encapsulative surface. These features can provide enhanced weather resistance, fire resistance, moisture absorption, jet blast resistance, improve their energy absorbing properties, or other desired features.

    Abstract translation: 本发明的实施方案涉及用作车辆制动系统（也称为工程材料拦阻系统（EMAS））的复合材料。具体实施方案可以使用改性聚合物泡沫复合材料。聚合物泡沫可以包括添加剂，涂料， 两者或其他特征，使其对于EMAS有用，聚合物泡沫也可以具有提供防护性外壳的一个或多个改性表面，例如，可以通过加热来改变一个或多个表面，以帮助关闭 这些特征可以提供增强的耐候性，耐火性，吸湿性，抗喷射性，提高其吸收能力或其他所需特征。

    JET BLAST RESISTANT VEHICLE ARRESTING BLOCKS, BEDS AND METHODS
    5.
    发明申请
    JET BLAST RESISTANT VEHICLE ARRESTING BLOCKS, BEDS AND METHODS 审中-公开
    喷气式电动车辆抵抗块，床和方法

    公开(公告)号：WO2003022682A1

    公开(公告)日：2003-03-20

    申请号：PCT/US2002/029253

    申请日：2002-09-13

    Applicant: ENGINEERED ARRESTING SYSTEMS CORPORATION ,  ALLEN, Glenn ,  ANGLEY, Richard, D. ,  GORDON, John, L. ,  MAHAL, Peter, T. ,  VALENTINI, Silvia, C.

    Inventor： ALLEN, Glenn ,  ANGLEY, Richard, D. ,  GORDON, John, L. ,  MAHAL, Peter, T. ,  VALENTINI, Silvia, C.

    IPC: B64F1/02

    CPC classification number: B64F1/025

    Abstract: Aircraft arresting beds (10) constructed of cellular concrete at ends of runways may be subject to damaging effects of jet blast phenomena. Arresting units resistant to such effects are described. A block of compressible material (12), such as cellular concrete, provides compressive failure characteristics suitable for arresting travel of an aircraft overrunning a runway. A top sheet (14) of relatively thin frangible material positioned above the block (12) provides a stronger, more damage resistant surface, while still readily fracturing in an arresting incident. Intermediate material (16), such as a foam layer, under the top sheet (14) may be included to provide a protective cushioning effect by mitigating transmission of external phenomena forces to the block (12). A wrapping (18), such as polyester net, at least partially enclosing other portions of the arresting unit provides a stable unified composite, without destroying desired compressive failure characteristics of the unit. Arresting units (10) may also include a bottom layer (20) of material stronger than the block of compressible material and a sealant coating with water resistant properties.

    Abstract translation: 在跑道末端由多孔混凝土构成的飞机拦截床（10）可能会受到喷气现象的破坏作用。 描述了抵抗这种效果的逮捕单位。 诸如多孔混凝土的可压缩材料块（12）提供适合于阻止超越跑道的飞机的行进的压缩破坏特性。 定位在块体（12）上方的相对较薄的易碎材料的顶片（14）提供更坚固，更具抗损伤性的表面，同时仍然容易地在止动事件中压裂。 可以包括在顶片（14）下方的诸如泡沫层的中间材料（16），以通过减轻对块（12）的外部现象力的传递来提供保护性缓冲效果。 至少部分地包围止动单元的其它部分的诸如聚酯网的包裹物（18）提供稳定的统一复合材料，而不破坏单元的期望的压缩破坏特性。 捕获单元（10）还可以包括比可压缩材料块更坚固的材料的底层（20）和具有防水性能的密封剂涂层。

    TAPE ELEVATION ADJUSTMENT DEVICE FOR AIRCRAFT ARRESTING SYSTEMS
    6.
    发明申请
    TAPE ELEVATION ADJUSTMENT DEVICE FOR AIRCRAFT ARRESTING SYSTEMS 审中-公开

    公开(公告)号：WO2019199390A1

    公开(公告)日：2019-10-17

    申请号：PCT/US2019/020366

    申请日：2019-03-01

    Applicant: ENGINEERED ARRESTING SYSTEMS CORPORATION

    Inventor： LEVESQUE, Christopher

    IPC: B64F1/02

    Abstract: Embodiments relate to aircraft arresting systems that use a net or a cable that extends across a section of a runway. Ends of the net or cable are secured to an elongated tape, which is secured to and forms a part of an energy absorbing brake system. The elongated tape is secured around a tape reel and is allowed to reel out (or "pay out") once the aircraft is engaged. Described is a system (10) for adjusting the height of the tape such that its elevation can be altered between the point at which it leaves the energy absorbing brake system and when it reaches the aircraft runway.

    ANCHORING SYSTEMS FOR AIRCRAFT ARRESTING NETS
    10.
    发明申请
    ANCHORING SYSTEMS FOR AIRCRAFT ARRESTING NETS 审中-公开
    航空器沉没网络的锚固系统

    公开(公告)号：WO2003043886A2

    公开(公告)日：2003-05-30

    申请号：PCT/US2002/032225

    申请日：2002-10-09

    Applicant: ENGINEERED ARRESTING SYSTEMS CORPORATION

    Inventor： COLARIK, David, K.

    IPC: B64F1/02

    CPC classification number: B64F1/02

    Abstract: Anchoring systems for aircraft arresting nets utilize frangible anchor links around lower horizontal straps of each net element of a composite arresting net. Each anchor link may be formed from flexible plastic sheet material, with openings through which an anchor cable passes and is secured to a runway surface by an anchor retainer. The anchor links provide ease of anchoring system assembly in the field and retain the bottom of the arresting net in proper position prior to engagement of the arresting net by an aircraft overrunning the runway. When an aircraft engages the net, the anchor links break to permit the net to conform to and safely stop the aircraft. Each anchor link may be perforated in its central portion or otherwise formed or specified to provide suitable frangibility in an arresting incident.

    Abstract translation: 用于航空器拦截网的锚固系统利用复合阻止网的每个网元的下水平带周围的易碎锚链。 每个锚连接件可以由柔性塑料片材料形成，具有开口，锚缆通过该开口，并且通过锚保持器固定到跑道表面。 锚链接提供了现场锚固系统组装的便利性，并且在通过超越跑道的飞机接合止动网之前将止动网的底部保持在适当的位置。 当飞机从事网络时，锚链断裂，以允许网络符合并安全停止飞机。 每个锚链节可以在其中心部分穿孔或以其他方式形成或指定以在逮捕事件中提供适当的脆弱性。

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